DE3934268A1 - Turbinen-staustrahltriebwerk - Google Patents
Turbinen-staustrahltriebwerkInfo
- Publication number
- DE3934268A1 DE3934268A1 DE19893934268 DE3934268A DE3934268A1 DE 3934268 A1 DE3934268 A1 DE 3934268A1 DE 19893934268 DE19893934268 DE 19893934268 DE 3934268 A DE3934268 A DE 3934268A DE 3934268 A1 DE3934268 A1 DE 3934268A1
- Authority
- DE
- Germany
- Prior art keywords
- engine
- flaps
- shut
- air
- casing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 238000011144 upstream manufacturing Methods 0.000 claims description 12
- 238000007906 compression Methods 0.000 claims description 3
- 230000006978 adaptation Effects 0.000 claims 1
- 238000005422 blasting Methods 0.000 claims 1
- 239000003570 air Substances 0.000 description 50
- 238000002485 combustion reaction Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 239000012080 ambient air Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000005253 cladding Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- CNKHSLKYRMDDNQ-UHFFFAOYSA-N halofenozide Chemical compound C=1C=CC=CC=1C(=O)N(C(C)(C)C)NC(=O)C1=CC=C(Cl)C=C1 CNKHSLKYRMDDNQ-UHFFFAOYSA-N 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
- F02K7/16—Composite ram-jet/turbo-jet engines
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19893934268 DE3934268A1 (de) | 1989-10-13 | 1989-10-13 | Turbinen-staustrahltriebwerk |
| FR9012620A FR2653177B1 (fr) | 1989-10-13 | 1990-10-12 | Turbo-statoreacteur equipant des avions pour vol sub et/ou hypersonique. |
| US07/597,035 US5094071A (en) | 1989-10-13 | 1990-10-15 | Turboramjet engine |
| JP2276142A JPH03194158A (ja) | 1989-10-13 | 1990-10-15 | タービンラムジェットエンジン |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19893934268 DE3934268A1 (de) | 1989-10-13 | 1989-10-13 | Turbinen-staustrahltriebwerk |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DE3934268A1 true DE3934268A1 (de) | 1991-04-25 |
| DE3934268C2 DE3934268C2 (enrdf_load_stackoverflow) | 1993-02-04 |
Family
ID=6391442
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19893934268 Granted DE3934268A1 (de) | 1989-10-13 | 1989-10-13 | Turbinen-staustrahltriebwerk |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US5094071A (enrdf_load_stackoverflow) |
| JP (1) | JPH03194158A (enrdf_load_stackoverflow) |
| DE (1) | DE3934268A1 (enrdf_load_stackoverflow) |
| FR (1) | FR2653177B1 (enrdf_load_stackoverflow) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2692938B1 (fr) * | 1992-06-24 | 1994-09-02 | Snecma | Réacteur combiné et muni de moyens de commutation entre deux états de fonctionnement. |
| TW274625B (enrdf_load_stackoverflow) * | 1994-09-30 | 1996-04-21 | Hitachi Seisakusyo Kk | |
| US5787703A (en) * | 1996-05-10 | 1998-08-04 | Fougerousse; Russell | Combined ramjet and rocket engine having rectilinear duct |
| US6089505A (en) | 1997-07-22 | 2000-07-18 | Mcdonnell Douglas Corporation | Mission adaptive inlet |
| US6883330B2 (en) * | 2002-10-02 | 2005-04-26 | United Technologies Corporation | Variable geometry inlet design for scram jet engine |
| US7721989B2 (en) * | 2006-03-01 | 2010-05-25 | The Boeing Company | Multi-path inlet for aircraft engine |
| USD614560S1 (en) | 2009-02-25 | 2010-04-27 | Alexander Charles R | Foreign object deflector |
| FR2967725B1 (fr) * | 2010-11-23 | 2012-12-14 | Snecma | Propulseur combine turboreacteur et statoreacteur |
| US9435219B2 (en) * | 2012-04-24 | 2016-09-06 | General Electric Company | Gas turbine inlet system and method |
| US11041463B1 (en) * | 2015-02-11 | 2021-06-22 | Raytheon Technologies Corporation | Turbine engine structure with oxidizer enhanced mode |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1271544A (fr) * | 1960-07-11 | 1961-09-15 | Nord Aviation | Combiné turboréacteur-statoréacteur |
| US3161379A (en) * | 1962-08-23 | 1964-12-15 | Bristel Siddeley Engines Ltd | Aircraft powerplant |
| GB971223A (en) * | 1962-12-17 | 1964-09-30 | Rolls Royce | Gas turbine power plant |
| FR1496091A (fr) * | 1966-04-20 | 1967-09-29 | Snecma | Tuyère d'éjection pour propulseurs à plusieurs flux moteurs, notamment à deux flux moteurs |
| FR1586188A (enrdf_load_stackoverflow) * | 1968-09-06 | 1970-02-13 | ||
| GB1361681A (en) * | 1971-04-07 | 1974-07-30 | Marconi Co Ltd | Radar systems |
| DE3912330A1 (de) * | 1989-04-14 | 1990-10-18 | Mtu Muenchen Gmbh | Integriertes turbo-staustrahltriebwerk |
-
1989
- 1989-10-13 DE DE19893934268 patent/DE3934268A1/de active Granted
-
1990
- 1990-10-12 FR FR9012620A patent/FR2653177B1/fr not_active Expired - Fee Related
- 1990-10-15 US US07/597,035 patent/US5094071A/en not_active Expired - Fee Related
- 1990-10-15 JP JP2276142A patent/JPH03194158A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| FR2653177A1 (fr) | 1991-04-19 |
| DE3934268C2 (enrdf_load_stackoverflow) | 1993-02-04 |
| JPH03194158A (ja) | 1991-08-23 |
| US5094071A (en) | 1992-03-10 |
| FR2653177B1 (fr) | 1995-02-03 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| OP8 | Request for examination as to paragraph 44 patent law | ||
| D2 | Grant after examination | ||
| 8364 | No opposition during term of opposition | ||
| 8339 | Ceased/non-payment of the annual fee |